Harichkin M.V.

Mechanics and Mathematics department of MSU, The control and navigation laboratory

This article deals with the new aeromagnetic compensation system developed on the classic aircraft magnetic-interference model extended by stochastic process. The last one is used for modeling of magnetic field anomaly and magnetic field gradient. The deviation parameters are obtained by solution of the standard linear estimation task. The main advantage of this method is that there are no artificial limitations, which are presented in other methods.